As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OP 16 MAINT CHECK, THE LT FWD ENTRY DOOR INTERIOR ANGLE WAS CRACKED IN RADIUS AT FWD UPPER PRESSURE STOP FITTING, FIRST STOP FITTING FROM TOP OF DOOR ON FWD SIDE. CONFIRMED BY NDT. STOP DRILLED CRACK AND REPAIRED PER SRM 52-05, FIG 31.